LAX91FA342

NTSB accident investigation · Piper PA 28-180 · Reno, NV · August 3, 1991

Accident · FatalField investigationFinal report
Date
August 2, 1991, 20:33 local (Aug 3, 1991, 03:33 UTC)
Place
Reno, NV
Injuries
3 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N5277LPiper PA 28-180
Weather
Visual (VMC) · Day
Status
Completed · report February 8, 1993
Report
Approved by Office Director
FAA report
19910802031539A
Case key
27019

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Failure of the pilot to maintain proper airspeed by employing an excessive angle of attack during the takeoff climb during a go-around resulting in an aerodynamic stall and subsequent inflight loss of control. Contributing to the accident was the pilot's poor approach planning, compensation for wind conditions and a high density altitude.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

In flight encounter with weatherApproach
Weather condition - high density altitude
Compensation for wind conditions - poorPilot in commandFactor
Lack of recent experience in type of aircraftPilot in command
Weather condition - tailwind
Loss of control - in flightGo-around (vfr)
Weather condition - high density altitudeFactor
Go-around - selectedPilot in command
Weather condition - crosswind
Airspeed - improperPilot in commandCause
Object - building(nonresidential)

Analysis

A Piper pa 28-180 collided with portable buildings on the airport after an in flight loss of control. The pilot reported having problems receiving radio transmissions. The air traffic control tower cleared the pilot to land on the rwy most into the wind. The airplane continued past the active rwy and approached a perpendicular rwy resulting in a quartering tailwind. The airplane overshot the final approach course of the perpendicular rwy and initiated a go-around. During the go-around witnesses observed the airplane not gaining altitude and at a slow airspeed. The witnesses also indicated the sound of the engine appeared normal. The airplane then turned right, into a quartering headwind, stalled, and descended vertically to the ground. The wind velocity at the time of the accident was 13 KTS. The density altitude was computed to be about 7,500 feet MSL. According to the pilot operating handbook for the Piper pa 28-180, the airplane should have been capable of a 375 foot per minute rate of climb.

Aircraft

Registration
N5277L
Reported as
Piper PA 28-180
Category
Airplane
Serial number
28-4576
Airframe hours
251
Engine
Lycoming O-360-A4A, 180 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Operator
Squadron 2
Registered owner
Niemann, David L.
Airworthiness certificate
Standard, Normal
Last inspection
Unknown · February 1, 1991 · 4,695 hours before
Departed
OAK · Oakland, CA
Airport
RNO · Reno, runway 16, 10,000 × 150 ft, concrete

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
35
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
450 total · 145 in this make and model · 369 as pilot in command · 9 in the last 90 days · 3 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 13 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 39 °F
Altimeter
30.00 inHg
Observed at
RNO, 1 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N5277L · 1

Matched to the same aircraft by N-number and date.